Fluid-Structure Interaction Simulation of the Edge-to-Edge Repair of the Mitral Valve in Functional and Degenerative States

Author(s):  
K. D. Lau ◽  
G. Burriesci ◽  
V. Díaz-Zuccarini

The most common dysfunction of the mitral valve (MV) is mitral valve regurgitation (MVR) which accounts for approximately 70% of native MV dysfunction [1]. During closure, abnormal amounts of retrograde flow enter the left atrium altering ventricular haemodynamics, an issue which can lead to cardiac related pathologies. MVR is caused by a variety of different mechanisms which are either degenerative (myxomatous degeneration) or functional (annular dilation or papillary muscle displacement) [2]. Correction of MVR is performed by repairing existing valve anatomy or replacement with a prosthetic substitute, however repair is preferred as mortality rates are reduced (2.0% against 6.1% for replacement) along with other valve related complications [3]. A common and popular method of repair is the edge-to-edge repair (ETER), which aims to correct MVR by surgically connecting the regurgitant region through reducing the inter-leaflet distance. Although MV function is improved in systole, induced stresses are significantly increased in diastole where the MV is typically in a low state of stress. In order to assess the effect of this technique in diastole, where the dynamics of both the MV and ventricular filling are disrupted it is required to use fluid-structure interaction (FSI) modelling techniques. Here a FSI model of the of the MV has been described, using this model the resulting induced stresses from the ETER in both functional and degenerative states of the MV have been simulated and assessed using the explicit finite element code LS-DYNA.

Prosthesis ◽  
2020 ◽  
Vol 2 (2) ◽  
pp. 65-75 ◽  
Author(s):  
Milan Toma ◽  
Daniel R. Einstein ◽  
Charles H. Bloodworth ◽  
Keshav Kohli ◽  
Richard P. Cochran ◽  
...  

Mitral regurgitation imposes a significant symptomatic burden on patients who are not candidates for conventional surgery. For these patients, transcatheter repair and replacement devices are emerging as alternative options. One such device is an intravalvular balloon or spacer that is inserted between the mitral valve leaflets to fill the gap that gives rise to mitral regurgitation. In this study, we apply a large-deformation fluid-structure interaction analysis to a fully 3D subject-specific mitral valve model to assess the efficacy of the intra-valvular spacer for reducing mitral regurgitation severity. The model includes a topologically 3D subvalvular apparatus with unprecedented detail. Results show that device fixation and anchoring at the location of the subject’s regurgitant orifice is imperative for optimal reduction of mitral regurgitation.


2013 ◽  
Vol 71 ◽  
pp. 417-425 ◽  
Author(s):  
Xingshuang Ma ◽  
Hao Gao ◽  
Boyce E. Griffith ◽  
Colin Berry ◽  
Xiaoyu Luo

2017 ◽  
Vol 47 ◽  
pp. 128-136 ◽  
Author(s):  
Hao Gao ◽  
Liuyang Feng ◽  
Nan Qi ◽  
Colin Berry ◽  
Boyce E. Griffith ◽  
...  

2014 ◽  
Vol 30 (12) ◽  
pp. 1597-1613 ◽  
Author(s):  
Hao Gao ◽  
Xingshuang Ma ◽  
Nan Qi ◽  
Colin Berry ◽  
Boyce E. Griffith ◽  
...  

Author(s):  
Milan Toma ◽  
Daniel R. Einstein ◽  
Charles H. Bloodworth ◽  
Richard P. Cochran ◽  
Ajit P. Yoganathan ◽  
...  

2010 ◽  
Vol 19 (3) ◽  
pp. 096369351001900
Author(s):  
G. Mohamed ◽  
C. Soutis ◽  
A. Hodzic

A numerical study into the dynamic behaviour of hybrid pressurised barrels manufactured from GLARE (Glass fibre Reinforced laminate) has been performed using the Arbitrary-Lagrangian-Eulerian (ALE) method that accounts for fluid structure interaction within the explicit finite element software RADIOSS. The results high-lighted the importance of the geometrical features of the closed barrel when assessing the shock wave propagation of the blast wave. Also the effect of pre-pressurisation was studied which proved significant in providing additional internal energy to the system. It was concluded that pressurisation should be accounted in all future studies to model the dynamic crack growth and structural integrity of typical aircraft structures subjected to blast.


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